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Aerodynamic and functional consequences of wing compliance

✍ Scribed by Andrew M. Mountcastle; Thomas L. Daniel

Book ID
106037243
Publisher
Springer
Year
2009
Tongue
English
Weight
602 KB
Volume
46
Category
Article
ISSN
0723-4864

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A quasi-steady scheme for the analysis of aerodynamic interaction between a propeller and a wing has been developed. The quasi-steady analysis uses a 3D steady vortex lattice method for the propeller and a 3D unsteady panel method for the wing. The aerodynamic coupling is represented by periodic loa